Propulsion System (PS) for Nanosatellite Platform

Orbital maneuvering of cubesat-class spacecraft.
Year of release: 2016
Guaranteed service life (years): 3
Estimated production / delivery time (months): 12
Flight qualification of the product: No
Possibility to adapt the product to customer requirements: Yes

Parameter Value
Stock of characteristic velocity for nanosatellite with weight up to 5 kg up to 25-30 m/s
The total mass of PS 1,3 kg
Minimum energy consumption 3 - 5 W
Maximum power consumption 12 W
Working body weight up to 0,2 kg
Supply voltage 5 - 12 V
Preparation time for start of the PS (preheating) 60 s
The maximum time of a single inclusion to generate thrust up to 1200 s
Electrothermal engine thrust 0,003 - 0,01 N
Overall dimensions 91 х 96 х 130 mm


Electrothermal propulsion unit for nanosatellite platform.

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